Combustor aerodynamic using radial swirler

A study has been conducted to investigate the flow pattern in a gas turbine combustion chamber by simulation and experimental approaches. Flow pattern inside a combustor is important to self sustain the flame, increase mixing of air and fuel, and increase combustion intensity. Aerodynamically curved...

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Butiran Bibliografi
Pengarang-pengarang Utama: Mohd Jaafar, Mohammad Nazri, Jusoff, Kamaruzaman, Osman, Mohamed Seroleh, Ishak, Mohamad Shaiful Ashrul
Format: Artikel
Diterbitkan: Academic Journals 2011
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Capaian Atas Talian:http://eprints.utm.my/44791/
Penanda-penanda: Tambah Penanda
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